IP Library Granted Patent US 8,033,503
Granted Patent B2
US 8,033,503 · App. 12/308,831 · Granted Oct 11, 2011

Pressure bulkhead for an aerospace fuselage

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Quick Facts
Patent No.
US 8,033,503
App. No.
12/308,831
Granted
Oct 11, 2011
Kind
B2
Abstract

A pressure bulkhead for an aerospace fuselage includes a bulkhead main portion having an approximately flat shape in unloaded state; and a frame supporting and connecting said bulkhead main portion to the fuselage; wherein said bulkhead main portion includes an airtight structure having a reticular component.

Claims (30)

1. A pressure bulkhead for an aerospace fuselage, comprising:

a bulkhead main portion having an approximately flat shape in an unloaded state; and

a frame supporting and connecting said bulkhead main portion to the fuselage;

wherein said bulkhead main portion comprises an airtight structure having a reticular component comprising ligament elements which are braided ligaments forming a cloth adapted to be airtight, wherein said cloth comprises one or more layers of standard fabrics stacked in a quasi orthotropic sequence, and

wherein said cloth comprises at least one portion of polar weaves forming an opening for an airtight passage of a conduit.

2. The pressure bulkhead according to claim 1 ,

wherein said frame is made of metallic and/or composite material.

3. The pressure bulkhead according to claim 2 ,

wherein said frame is made of aluminium 7150.

4. The pressure bulkhead according to claim 1 ,

wherein said ligament elements are made of aromatic polyamide fibres.

5. A pressure bulkhead for an aerospace fuselage, comprising:

a bulkhead main portion having an approximately flat shape in an unloaded state; and

a frame supporting and connecting said bulkhead main portion to the fuselage;

wherein said bulkhead main portion comprises an airtight structure having a reticular component comprising ligament elements, and

wherein said ligament elements are belt-shaped ligaments extending radially in at least one first layer and one second layer, respectively and form at least two retaining layers for a sealing element arranged between said retaining layers.

6. The pressure bulkhead according to claim 5 ,

wherein said sealing element is a thermoplastic membrane.

7. The pressure bulkhead according to claim 5 ,

wherein inner ends of said belt-shaped ligament elements are connected to at least one central belt and the other ends are connected to at least one peripheral belt.

8. The pressure bulkhead according to claim 7 ,

wherein said sealing element is connected to said at least one peripheral belt.

9. The pressure bulkhead according to claim 7 ,

wherein said at least one peripheral belt is attached to said frame fixing said sealing element and said airtight structure having a reticular component to said frame.

10. The pressure bulkhead according to claim 5 ,

wherein said frame is made of metallic and/or composite material.

11. The pressure bulkhead according to claim 10 ,

wherein said frame is made of aluminium 7150.

12. The pressure bulkhead according to claim 5 ,

wherein said ligament elements are made of aromatic polyamide fibres.

Assignments (2)
CHANGE OF NAME Recorded May 31, 2011
From: AIRBUS DEUTSCHLAND GMBH
To: AIRBUS OPERATIONS GMBH
Reel/Frame 026360/0849 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 24, 2008
From: BASSO, PASQUALE
To: AIRBUS DEUTSCHLAND GMBH
Reel/Frame 022051/0600 →